Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:aircraftType |
low-wing monoplane
|
| gptkbp:built |
composite
|
| gptkbp:category |
gptkb:trainer_aircraft
civil utility aircraft |
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:crew |
2
|
| gptkbp:emptyWeight |
770 kg
|
| gptkbp:engine |
gptkb:Lycoming_AEIO-360
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1991
|
| gptkbp:height |
2.73 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Grob G 120A
|
| gptkbp:landingGear |
gptkb:cyclist
|
| gptkbp:length |
7.70 m
|
| gptkbp:manufacturer |
gptkb:Grob_Aircraft
|
| gptkbp:maximumSpeed |
235 km/h
|
| gptkbp:maxTakeoffWeight |
990 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:range |
900 km
|
| gptkbp:role |
gptkb:trainer_aircraft
|
| gptkbp:serviceCeiling |
4000 m
|
| gptkbp:usedBy |
gptkb:French_Air_Force
gptkb:Israeli_Air_Force gptkb:German_Air_Force gptkb:Canadian_Air_Force |
| gptkbp:wingspan |
10.00 m
|
| gptkbp:bfsParent |
gptkb:Israeli_Air_Force_Flight_Academy
|
| gptkbp:bfsLayer |
7
|